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_aSpringerLink (Online service) _9106996 |
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| 999 |
_c111043 _d111043 _x1 |
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| 001 | 111043 | ||
| 003 | ES-MaUEC | ||
| 005 | 20230102113451.0 | ||
| 006 | a||||fo|||| 00| 0 | ||
| 007 | cr nn nnnaamaa | ||
| 008 | 190319s2019 si a s |||| 0|eng d | ||
| 020 | _a9789811361302 | ||
| 024 | 7 |
_a10.1007/978-981-13-6130-2 _2doi |
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| 040 |
_bspa _dES-MaUEC |
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| 050 | 4 |
_aTL1050 _b2019 EB |
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| 100 | 1 |
_aYuan, Jianping. _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut |
|
| 245 | 1 | 0 |
_aLow Energy Flight : _bOrbital Dynamics and Mission Trajectory Design _cby Jianping Yuan, Yu Cheng, Jinglang Feng, Chong Sun |
| 264 | 1 |
_aSingapore _bSpringer Singapore : _bImprint: Springer _c2019. |
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| 300 |
_a1 recurso en línea (X, 209 páginas) _b 136 ilustraciones, 108 ilustraciones a color |
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| 347 |
_atext file _bPDF |
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| 490 | 0 | _aEngineering (Springer-11647) | |
| 505 | 0 | _aIntroduction -- Continuous Low Thrust Trajectory Design and optimization -- Study of the Transfer Between Libration Point Orbits and Lunar Orbits in Earth-Moon System -- Lorentz Force Formation Flying in Earth-Moon System -- Orbital Dynamics in the Irregular Gravitational Field - Resonance -- Orbital Dynamics in the Vicinity of Contact Binary Asteroid Systems -- Appendices. | |
| 520 | 3 | _aThe book focuses on the orbital dynamics and mission trajectory (transfer or target trajectory) design of low-energy flight in the context of modern astrodynamics. It investigates various topics that either offer new methods for solving classical problems or address emerging problems that have yet to be studied, including low-thrust transfer trajectory design using the virtual gravity field method; transfer in the three-body system using invariant manifolds; formation flying under space-borne artificial magnetic fields; and the orbital dynamics of highly irregular asteroids. It also features an extensive study of the orbital dynamics in the vicinity of contact binary asteroids, including the 1:1 ground-track resonance, the equilibrium points and their stability, and the third-order analytical solution of orbital motion in the vicinity of the non-collinear equilibrium point. Given its breadth of coverage, the book offers a valuable reference guide for all engineers and researchers interested in the potential applications of low-energy space missions. . | |
| 650 | 7 |
_aAstrodinámica _9488700 _2embne |
|
| 700 | 1 |
_aCheng, Yu. _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut |
|
| 700 | 1 |
_aFeng, Jinglang. _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut |
|
| 700 | 1 |
_aSun, Chong. _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut |
|
| 776 | 0 | 8 |
_iPrinted edition: _z9789811361296 |
| 776 | 0 | 8 |
_iPrinted edition: _z9789811361319 |
| 856 | 4 | 0 |
_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-981-13-6130-2 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid) |
| 942 | _2lcc | ||
| 988 | _aPrimersemestre_2019_Engineering | ||
| 998 |
_aSI _b09/2019 _cm _dz _ea _feng _ggw _h0 |
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